A two phase program was conducted to define requirements and to prepare a preliminary design of a test motor system that will accurately and economically simulate the chamber environments of present and future large solid propellant rocket motors. A segmented motor configuration with 28-in. outside diameter case bonded propellant grains was selected. The nominal grain configuration is an internal burning cylinder with both ends burning.
Ballistic Missile Propellant Evaluation Test Motor System (Super BATES)
1974
219 pages
Report
Keine Angabe
Englisch
Space technology - Third test of Fleet Ballistic Missile rocket motor
Online Contents | 2000
NTIS | 1966
|Missile guidance system against a ballistic missile
AIAA | 1991
|